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Graphical method of obtaining theoretical lift distributions on thin wings at supersonic speeds
Document ID
19930082314
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cohen, Clarence B
Evvard, John C
Date Acquired
August 16, 2013
Publication Date
August 1, 1948
Report/Patent Number
NACA-TN-1676
Report Number: NACA-TN-1676
Accession Number
93R11604
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THEORIES - FLOW SUPERSONIC
THEORIES - WINGS
WINGS, TRAPEZOIDAL
LIFT DISTRIBUTION - WING TIPS
THEORIES - FLOW LINEAR
LIFT DISTRIBUTION - WINGS, THIN

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